Boeing 727-2A1

Service difficulty reports · 502

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '7272A1'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SCNA98090Line · rupturedAFTER DEPARTURE LOSS OF A SYSTEM HYDRAULIC QUANTITY UPON GEAR RETRACTION. PERFORMED ALL COM PROCEDURES AND DUMPED FUEL. RETURNED TO MSP. FOUND RUPTURED LINE ON ELEVATOR ACCESSORY. REMOVED AND REPLACED LINE WITH FOLLOWING LEAK AND OPERATIONAL CHECKS GOOD.Aug 19, 1998 · N286SC · Boeing 7272A1 · Hydraulic System, MainSDR SCNA98069Connector · looseDURING CLIMB, THE NUMBER TWO ENGINE CSD TEMPERATURE INDICATION WAS LOST. THE NUMBER ONE CSD TEMP CLIMBED INTO THE YELLOW ARC AND THE NUMBER THREE ENGINE CSD TEMPERATURE INDICATION WAS ON MEL. AIR RETURNED INTO IAH. FOUND CANNON PLUG LOOSE ON OUT TEMPERATUREJul 5, 1998 · N287SC · Boeing 7272A1 · Alternator-Generator DriveSDR SCNA98043Gearbox · crackedDURING CRUISE FLIGHT, NUMBER TWO ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE DROPPED TO 25 PSI WITH THE QUANTITY DOWN TO .8 GALLONS. SHUT DOWN NUMBER TWO ENGINE AND DIVERTED TO DEN. REMOVED AND REPLACED NUMBER TWO ENGINE MAIN ACCESSORY GEARBOXMay 12, 1998 · N287SC · Boeing 7272A1 · Turbine Engine Accessory DriveSDR SCNA98036Wire · brokenEMERGENCY TRACK LIGHT AT ROW 18C IS INOPERATIVE. REPAIRED BROKEN WIRING AND FUNCTIONALLY CHECKED GOOD.Apr 21, 1998 · N287SC · Boeing 7272A1 · Light System WiringSDR UPS98225724Skin · corrodedINSPECTION TYPE:SI CORROSION (C53-224-01.00-02) ON INTERIOR OF SKIN AROUND PERIMETER OF SIDELIGHT BETWEEN BS 720B PLUS 5 AND 720C LBL 73 WL 218-228 BETWEEN STR 14L AND 16L. CORROSION OUT OF LIMITS IAW SRM 53-30-3. REPAIRED SKIN AROUND PERIF OF LT SIDELIGHT IFeb 5, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR UPS98225711Rib · corrodedINSPECTION TYPE-SI, FRETTING CORROSION ON VERTICAL STAB L/E FAIRING RIB, FWD LIP AT FIN STA 55.9. RECEIVED NEW TEE-EXTRUDED RIB AND INSTALLED WEB TO NEW RIB PER 727 SRM 51-30-2.Feb 2, 1998 · N214UP · Boeing 7272A1 · Vertical Stabilizer, Spar/RibSDR UPS98225664Bottle Pin · corrodedINSPECTION TYPE-SI, R/W REAR BOTTLE PIN IS CORRODED. ALSO, FWD AND AFT BUSHINGS ARE MISSING SECTION OF MICARTA INNER SLEEVE CORROSION (C53-100-05.00-04). REMOVED AND REPLACED R/W AFT BOTTLE PIN ON NRC 657574 IAW MM 57-41-01, BUSHING REPLACED ON AOG (BOEING) Jan 27, 1998 · N214UP · Boeing 7272A1 · Wing, Fuselage Attach FittingsSDR UPS98225663Rear Spar · crackedINSPECTION TYPE-SI, L/W STRINGER 2ND FROM REAR SPAR ON UPPER SKIN AT WING STATION 686.5 IS CRACKED AT STRINGER 5 TO 10. REPAIRED L/W STRINGER 2ND FROM REAR SPAR (STR 10) AT STA 686.5 IAW UPS EO B727-5710-0314.Jan 27, 1998 · N214UP · Boeing 7272A1 · Wing SparSDR UPS98225709Support · corrodedINSPECTION TYPE-SI, NR 7 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT AFT BOLT HOLES FLAP TRACK FWD ATTACH POINT BUSHING HAS MIGRATED. ALSO, FWD HARDWARE REQUIRES REPLACEMENT I/B AND O/B AT RADIUS BLOCKS. REPLACED NR 7 FLAP TRACK FITTING IAW SRM 51-10-1 WILLJan 22, 1998 · N214UP · Boeing 7272A1 · Trailing Edge FlapsSDR UPS98225710Support · corrodedINSPECTION TYPE-SI, NR 4 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT FLAP TRACK FWD ATTACH LUG I/B SIDE. REMOVED AND REPLACED NR 4 FLAP TRACK FWD FITTING IAW MM 32-11-51.Jan 18, 1998 · N214UP · Boeing 7272A1 · Trailing Edge FlapsSDR SCNA98014Keel Beam · crackedDURING A SCHEDULED MAINTENANCE CHECK, A CRACK WAS LOCATED ON THE VERTICAL KEEL BEAM CHORD AT BS 870, APPROXIMATE RBL 3.5. DURING REMOVAL AND REPLACEMENT OF THE CRACKED CHORD A KEEL BEAM SUPPORT ANGLE WAS FOUND CRACKED COMPLETELY THROUGH BOTH FLANGES AND A CRAJan 18, 1998 · N287SC · Boeing 7272A1 · Fuselage Main, KeelSDR SCNA98013Keel Beam · crackedDURING A SCHEDULED MAINTENANCE CHECK, A CRACK WAS LOCATED ON THE VERTICAL KEEL BEAM CHORD AT BS 870, APPROXIMATE RBL 3.5. DURING REMOVAL AND REPLACEMENT OF THE CRACKED CHORD NO ADJACENT STRUCTURE WAS FOUND DAMAGED.Jan 18, 1998 · N286SC · Boeing 7272A1 · Fuselage Main, KeelSDR UPS98225496Sill · crackedINSPECTION TYPE-SI, MOPSILL CRACKED LBL 54 STA 294 TO 304 WL 208. REPLACED MOPSILL AT LBL 54 STA 294 TO 304 WL 208 IAW SRM 51-30-2.Jan 16, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS98225497Beam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON LONGITUDINAL BEAM ST 760 TO 848 LBL 45 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED LONGITUDINAL BEAM IAW SRM 51-10-1, 51-30-2.Jan 15, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS98225495Stringer · crackedINSPECTION TYPE-SI, DISCOVERED END OF STR 15L TO BE CRACKED AT BS 720+5. AREA OF DAMAGE REMOVED AND STRINGER END REPAIRED PER SRM 53-10-3 AND SRM 51-30-2.Jan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Longeron/StringerSDR UPS98225478Skin · corrodedINSPECTION TYPE-SI, WHILE CLOSING FLOOR ON CARD 656802 FOUND CORROSION ON SKIN AT BS 1090 AT STR 28R. REMOVED CORROSION IAW SRM 51-10-6 REWORK OUT OF LIMITS IAW SRM 53-30-1. REPAIRED SKIN AT STA 1090 STR 28R IAW SRM 53-30-3.Jan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Plate/SkinSDR UPS98225477Chord · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-03) ON NUT PLATE AND FLOORBEAM AT STA 1166, LBL 10, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REPAIRED FLOORBEAM PER SRM 53-10-8.Jan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS98225473Angle · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT MOP SILL AT BOTTOM OF RT ENTRY DOOR BS 380 TO 410 RBL 63 WL 208 TOP AND BOTTOM SURFACES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON LWR SUPPORT ANGLE IAW 51-10-06, 53-10-1. REMOVED AND REPLACED ANGLE IAJan 14, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS98225472Seat Track · corrodedINSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK FLANGE BETWEEN BS 720D TO 720F LBL 25. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK BS 720D TO BS 720F LBL 25 IAW SRM 53-10-5.Jan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225470Frame · crackedINSPECTION TYPE-SI, CRACK INDICATION NOTED AT FASTENER HOLE IN FRAME AT BS 783.95 APPROX WL 207 APPROX LBL 65. REPAIRED CRACK IN FRAME STA 783.95 LBL 65 WL 207 IAW UPS EO B727-5310-5474.Jan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, FrameSDR UPS98225469Seat Track · corrodedINSPECTION TYPE-SI, CORROSION (4-25-02) AND MECHANICAL DAMAGE ON SEAT TRACK WELL AND TOOTH BETWEEN BS 980 TO 1010 LBL 25. CORROSION REWORK OUT OF LIMTS IAW SRM 53-10-1. MECHANICAL DAMAGE WITHIN LIMITS IAW SRM 53-10-1. SEAT TRACK WAS REMOVED AND REPLACED IAWJan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225468Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON TOP OF FLOORBEAM 950 RBL 25 TO 65. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPAIRED 950 FLOORBEAM RBL 25 TO 65 IAW TRAMCO/BFG EWO 98-2012 (UPS FILE 727-53-1983).Jan 13, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS98225467Lug · corrodedINSPECTION TYPE-SI, NR 4 K-FLAP HAS CORROSION ON O/B UPPER LUG WHERE BONDING JUMPER ATTACHES. REMOVED AND REPLACED NR 4 K-FLAP IAW OHM 57-51-21 AND MM 27-81-01.Jan 12, 1998 · N214UP · Boeing 7272A1 · Leading Edge DevicesSDR UPS98225466Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION AT BS 380 RBL 45 TO 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AND BOTTOM SURFACE AT FASTENER HOLES (C53-224-01.05-01). CORROSION REMOVED IAW SRM 51-10-6 OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FLOORBEAM IAW SRM 53-10-8.Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS98225465Seat Track · corrodedINSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 720C TO BS 745 RBL 25, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED CORRODED SEAT TRACK, FABRICATED, INSTALLED REPAIR SEAT TRACK IAW SRM 53-10-5.Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225464Seat Track · corrodedINSPECTION TYPE-SI, CORROSION (2-224-01) GOUGES AND BARE METAL ON SEAT TRACK AT BS 520 BS 610, LBL 60, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-05, 51-30-08, MM 51-20-31, OHM 20-50-01Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225463Link · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.00-02) ON EXPANSION LINK AT BS 740 TO 755 LBL 45. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED LINK PER SRM 51-20-1, 51-10-1, 51-30-2.Jan 12, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS98225404Frame · corrodedINSPECTION TYPE-SI, CORROSION ON FRAME BS 720D STR 10 TO 13 RT. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.Jan 9, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, FrameSDR UPS98225403Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE UNDER NUT PLATES BS 1070, BL 0 TO LBL 10 WL 200. REMOVED DAMAGED SECTION AND REPAIRED LOWER FLANGE IAW SRM 53-10-8.Jan 9, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS98225462Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT BS 480 LBL 45 RBL 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AS MARKED. CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8.Jan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS98225461Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON TOP CHORD OF FLOORBEAM AT BS 620 RBL 10 WL 208. CORROSION ON CHORD FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS PER SRM 53-10-8.Jan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS98225460Seat Track · dentedINSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 484 TO BS 570 BL 0 WL 208. CORROSION ON SEAT TRACK WAS FOUND TO BE WITHIN LIMITS AFTER CLEAN UP. HOWEVER, DENTS WERE FOUND ON BS 490 AND BS 571 WHICH WERE OUT OF LIMITS. SEAT TRACK WAS REPLACED FROJan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR UPS98225397Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE AT NUT PLATE BS 950F, LBL 12, WL 200. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER AND TRIPLER ANGLE AND FILLER IAW SRM 53-10-8.Jan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR UPS98225396Frame · dentedINSPECTION TYPE-SI, AFT CARGO BAY BS 1130 AT STR 26L FRAME IS DENTED. DENT FOUND OUT OF LIMITS PER SRM 51-30-1. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-40-3 AND SRM 51-30-2.Jan 8, 1998 · N214UP · Boeing 7272A1 · Fuselage Main, FrameSDR SCNA98009Strap · out of positionAIR RETURN DUE TO DOOR STRAP NOISE FROM DOOR 2R. REMOVED DOOR STRAP FROM DOOR AND INSPECTED DOOR SKIN AND NR 3 ENGINE C1 AND C2 DISCS FOR DAMAGE. NO DAMAGE FOUND AND OPS CHECK OK.Jan 5, 1998 · N286SC · Boeing 7272A1 · Passenger/Crew DoorsSDR UPS98225662Fitting · corrodedINSPECTION TYPE-SI, RIGHT WING NR 5 FLAP TRACK FWD ATTACH FITTING I/B SIDE CORRODED (CORROSION C57-581-07.00-04). CORROSION FOUND TO BE OUT OF LIMITS PER SRM 57-40-01. REPLACED WITH NEW FITTING IAW MM 32-11-51 AND OHM 20-50-03.Jan 4, 1998 · N214UP · Boeing 7272A1 · Trailing Edge FlapsSDR UPS98225518Beam Block · corrodedINSPECTION TYPE:SI NR 3 FLAP TRACK REAR SPAR ATTACH POINT HAS CORROSION, ALSO BOTH FAIL/SAFE ATTACH HOLES. FLAP TRACK BEAM BLOCK REMOVED, FOUND OUT OF LIMITS AND REPLACED WITH NEW ITEM PER SRM 57-30-5, 51-10-2 AND 51-30-2.Jan 4, 1998 · N214UP · Boeing 7272A1 · Trailing Edge FlapsSDR UPS98225494Sill · corrodedINSPECTION TYPE-SI, CORROSION (C53-224-01.05-03) ON MOPSILL BETWEEN BS 950 TO 950A, LBL 65 AROUND NUT PLATE HOLES. MOPSILL BS 950 TO 950A FOUND TO BE OUT OF LIMITS SRM 51-40-4. REMOVED CORRODED AREA IAW SRM 53-10-1, FABRICATED AND INSTALLED REPAIR PARTS SRM Jan 4, 1998 · N214UP · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR UPS98225402Bonding Jumper · corrodedINSPECTION TYPE-SI, NR 5 K-FLAP O/B LOWER BONDING JUMPER HAS CORROSOION WHERE JUMPER ATTACHES. CORROSION FOUND OUT OF LIMITS PER SRM 57-50-01. CORROSION DAMAGE REMOVED AND STANDARD REPAIR COMPLETED PER SRM 57-50-3, SRM 51-20-2 AND SRM 51-30-00.Jan 2, 1998 · N214UP · Boeing 7272A1 · Leading Edge DevicesSDR UPS98225723Fitting · corrodedINSPECTION TYPE:SI NR 8 FLAP TRACK FWD ATTACH FITTING IS CORRODED AROUND FLAP TRACK FWD ATTACH POINT BUSHING, AND BUSHING MIGRATED AND CORROSION IN FAIL/SAFE STRAP ATTACH POINT BOLT HOLES FWD ATTACH HARDWARE REQUIRES REPLACEMENT OUTBOARD AND INBOARD. REWORKEDJan 1, 1998 · N214UP · Boeing 7272A1 · Trailing Edge FlapsSDR UPS98225661Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) AFT CARGO BAY ON FLOORBEAM, FWD LOWER UNDER NUT PLATES BS 1130, LBL 6 TO LBL 25, WL 200. CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIR BY ADDITION OF REPAIR ANGLES PER BOEING TELEX TCO-PAN-98-07175RR ADec 31, 1997 · N214UP · Boeing 7272A1 · Fuselage Main, Floor BeamSDR SCNA97355Support · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND THE FLOOR SUPPORT CHANNEL AT STATION 344, RBL 50 - 62.5 CORRODED OUT OF LIMITS. REMOVED, FABRICATED, AND INSTALLED NEW CHANNEL IAW SRM 51-30-2, 51-20-2, 51-10-1 AND DRAWING 65-26173.Nov 9, 1997 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR SCNA97360Floorbeam · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND THE FLOORBEAM UPPER CAP CORRODED BEYOND LIMITS AT STATION 344, RBL 68 - LBL 52. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CAP IAW SRM 51-10-1, AND 51-10-2.Nov 8, 1997 · N286SC · Boeing 7272A1 · Fuselage Main, Floor BeamSDR SCNA97358Seat Track · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND THE SEAT TRACK AT STATION 344-360, LBL 22 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW SRM 51-30-2, 53-10-5, AND 51-10-2.Nov 8, 1997 · N286SC · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR SCNA97357Seat Track · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND THE SEAT TRACK AT STATION 344-380, RBL 44 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW SRM 51-30-2.Nov 8, 1997 · N286SC · Boeing 7272A1 · Fuselage, Seat/Cargo Attach FittingsSDR SCNA97359Support · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND FLOORBOARD SUPPORT CHANNEL IN THE AFT CARGO PIT DENTED AND PUNCTURED FROM STATION 950E TO 990. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT CHANNEL IAW SRM 53-10-2 AND 51-30-01.Nov 5, 1997 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR SCNA97356Support · corrodedDURING HEAVY MAINTENANCE VISIT, FOUND THE FLOORBOARD SUPPORT CHANNEL IN THE AFT CARGO PIT DENTED AT STATION 950F, RBL 11. REMOVED, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-30-02, 53-10-2, AND 51-30-2.Nov 5, 1997 · N286SC · Boeing 7272A1 · Fuselage Miscellaneous StructureSDR SCNA97342Bushing · out of adjustAT APPROXIMATELY 14,000 FT ALTITUDE AND 314 KNOTS INDICATED, AIRCRAFT VIBRATION WAS PRESENT. THE RIGHT INBOARD TRAILING EDGE FLAP WAS DISCOVERED TO BE VIBRATING. DUMPED FUEL AND RETURNED TO LAS. FOUND AFT AND FWD ROLLER BEARINGS ON RT INBD FLAP WITH EXCESSIOct 17, 1997 · N287SC · Boeing 7272A1 · Trailing Edge FlapsSDR UPS97224629Batteries · dischargedINSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE WHEN SELECTED ON. REPLACED 4 EA DEAD BATTERIES S106 EMERGENCY EXIT LIGHTS, OPS CK GOOD.Oct 7, 1997 · N214UP · Boeing 7272A1 · Emergency LightingSDR UPS97224519Skin · crackedF/S 1130 LBL 20 AFT BELLY SKIN CRACK 1.0 INCH LONG WITH BULGE. VERIFIED CRACK WITH EDDY CURRENT, FOUND TO BE FWD AND AFT BETWEEN TWO RIVETS. REMOVED CORROSION AS REQUIRED, CLEANED STRINGER FOR INSPECTION (3) REMAINING STEPS TO BE COMPLETED ON A WIP FORM ACCSep 23, 1997 · N214UP · Boeing 7272A1 · Fuselage Main, Plate/Skin
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